发明公开
EP1834076A1 TIP TURBINE ENGINE COMPRISING TURBINE BLADE CLUSTERS AND RADIAL ATTACHMENT LOCK ARRANGEMENT THEREFOR
有权
为这样的基团的组件的风扇转子的方法和涡轮机叶片簇
- 专利标题: TIP TURBINE ENGINE COMPRISING TURBINE BLADE CLUSTERS AND RADIAL ATTACHMENT LOCK ARRANGEMENT THEREFOR
- 专利标题(中): 为这样的基团的组件的风扇转子的方法和涡轮机叶片簇
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申请号: EP04822123.8申请日: 2004-12-01
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公开(公告)号: EP1834076A1公开(公告)日: 2007-09-19
- 发明人: SUCIU, Gabriel L. , NORRIS, James W. , NORDEEN, Craig A.
- 申请人: United Technologies Corporation
- 申请人地址: One Financial Plaza Hartford CT 06101 US
- 专利权人: United Technologies Corporation
- 当前专利权人: United Technologies Corporation
- 当前专利权人地址: One Financial Plaza Hartford CT 06101 US
- 代理机构: Leckey, David Herbert
- 国际公布: WO2006060009 20060608
- 主分类号: F02K3/068
- IPC分类号: F02K3/068 ; F02C3/073 ; F02C3/08 ; F01D5/22 ; F01D5/30
摘要:
A tip-turbine engine comprises a fan-turbine rotor assembly that includes one or more turbine ring rotors. Each turbine ring is assembled from a multitude of turbine blade clusters. By forming the turbine blades in clusters, leakage between adjacent blade platforms is minimized which increases engine efficiency. Assembly of the turbine blade clusters to a diffuser surface includes axial installation and radial locking of each turbine blade cluster. This is accomplished by attachment lugs protruding from the underside of the arcuate base of the turbine blade clusters. Torque load surfaces are also integrated into the arcuate base.
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